System and methods for airborne launch and recovery of aircraft

Abstract

A system and methods for airborne launch and recovery of aircraft. In one embodiment the system comprises a flexible tether configured to be towed behind an airborne mother ship. A drag device is secured to a distal end of the flexible tether to generate drag and maintain tension in the flexible tether. A reel associated with the mother ship anchors a proximal portion of the flexible tether and selectively lets out and takes up the flexible tether to adjust a length of the flexible tether. A capture mechanism associated with the aircraft engages the flexible tether to enable the aircraft to translate along the flexible tether. In embodiments of the present methods, a flexible tether is deployed from an airborne mother ship. An aircraft translates forward and rearward along the flexible tether. Prior to launch, the weight of the aircraft is transferred from the flexible tether to the wings. During recovery, the weight of the aircraft is transferred from the wings to the flexible tether.

Description

BACKGROUND[0001]1. Technical Field[0002]The present disclosure relates to aircraft.[0003]2. Description of Related Art[0004]In modern warfare tactical aircraft are an indispensable asset to military commanders. However, tactical aircraft are limited by, for example, fuel capacity, weaponry capacity and configuration, and maintenance intervals. In-flight refueling can extend combat operations. However, aircraft must still return to a ground base to rearm and to have maintenance performed. Similarly aircraft used in civilian applications such as crop-dusting, aerial police / traffic surveillance, and countering man-portable air-defense systems are also limited by their need to return to ground for maintenance, reconfiguration, etc.[0005]These limitations are exacerbated in unmanned air vehicles (UAVs) and unmanned combat air vehicles (UCAVs). For simplicity, the abbreviation UAV will be used herein to refer to both unmanned air vehicles and unmanned combat air vehicles. With the advent ...

AI Technical Summary

Benefits of technology

The present patent describes a system and methods for airborne launch and recovery of aircraft. The system includes a flexible tether towed behind an airborne mother ship and a drag device to maintain tension in the tether. The tether is selectively let out and taken up by a reel on the mother ship. The system also includes a capture mechanism associated with the aircraft to engage the tether during launch and recovery. The methods involve deploying the tether, translating the aircraft along the tether, and transferring the weight of the aircraft from the tether to the wings or vice versa. The technical effects of this system include the ability to launch and recapture aircraft, extend the missions of each aircraft, and smoothly recover and launch aircraft without being affected by turbulent airflow near the mother ship.

Problems solved by technology

However, tactical aircraft are limited by, for example, fuel capacity, weaponry capacity and configuration, and maintenance intervals.

Similarly aircraft used in civilian applications such as crop-dusting, aerial police / traffic surveillance, and countering man-portable air-defense systems are also limited by their need to return to ground for maintenance, reconfiguration, etc.

These limitations are exacerbated in unmanned air vehicles (UAVs) and unmanned combat air vehicles (UCAVs).

But tactical UAVs configured for high endurance typically achieve endurance at the expense of speed and range, thus limiting the spectrum of situations in which they can be deployed.

Historically, however, attempts at airborne recovery of aircraft have met with little, if any, success.

However, even these moderate successes failed to solve the major problems associated with traditional trapeze- or arm-based airborne recovery, in which the recovered aircraft's weight must be transitioned from its own lift to the mother ship.

The transition typically happens close to the mother ship, due to the length of the recovery device, requiring the difficult connection to be made as the deployed aircraft transitions from “clean” air, to a turbulent wake and boundary layer surrounding the mother ship and finally to dead air where it cannot create sufficient lift for flight.

These transitions through different types of air make it very difficult to control the aircraft being recovered.

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